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PID LQR control for a quadrotor: Modeling and simulation

机译:四旋翼飞机的PID和LQR控制:建模和仿真

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This paper aims to present a comparison between various controllers to be used in dynamic model of a quadrotor platform. The controllers assumed in this work are conventional PID and a classic LQR controller. The PID controller is chosen for quadrotor model because of its versatility and facile implementation, while also providing a good response for the model dynamics attitudes. The LQR controller seemed to be a good comparative controller due to its great performance and robustness in the plant. In this study, it is accomplished that both the controllers provide satisfactory feedback for quadrotor stabilization.
机译:本文旨在介绍用于四旋翼平台动力学模型的各种控制器之间的比较。在这项工作中假设的控制器是传统的PID和经典的LQR控制器。 PID控制器之所以被选择用于四旋翼模型,是因为其多功能性和便捷的实现方式,同时还为模型动力学姿态提供了良好的响应。由于LQR控制器在工厂中具有出色的性能和鲁棒性,因此它似乎是一个很好的比较控制器。在这项研究中,可以实现两个控制器都为四旋翼稳定器提供令人满意的反馈。

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